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Design and performance of small nuclear stages compatible with small and intermediate class launch vehicles

机译：与中小型运载火箭兼容的小型核动力级的设计和性能

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作者
Kiersarsky, A. S.; Osias, D. J.; Skeer, M. H.;
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年度 1969
页码 1-39
总页数 39
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
LAUNCH VEHICLES; NUCLEAR PROPULSION; NUCLEAR ROCKET ENGINES; CRYOGENIC ROCKET PROPELLANTS; INTERPLANETARY SPACECRAFT; PARKING ORBITS; PAYLOADS;

机译：发射车辆;核武器推进;核弹簧发动机;低温火箭推进剂;行星际航天器;停车轨道;有效载荷;

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4. FEASIBILITY OF NUCLEAR SINGLE STAGE TO ORBIT, REUSABLE LAUNCH VEHICLE [C] . Kyle Vacca, Andrea Johnson 55th International Astronautical Congress 2004 vol.10 . 2004

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7. Feasibility of SCRAMJET technology for an intermediate propulsive stage of an expendable launch vehicle [O] . Schafer Michael D. 2002

机译：SCRAMJET技术在消耗性运载火箭的中间推进阶段的可行性

Design and performance of small nuclear stages compatible with small and intermediate class launch vehicles

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